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Gas Turbine Handbook : Principles and Practices

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80 <strong>Gas</strong> <strong>Turbine</strong> <strong>H<strong>and</strong>book</strong>: <strong>Principles</strong> <strong>and</strong> <strong>Practices</strong><br />

down, thereby lowering the compressor speed as well as airflow <strong>and</strong><br />

pressure. The downward spiral continues until the desired shaft<br />

horsepower is reached.<br />

While it is possible to increase <strong>and</strong> decrease shaft horsepower<br />

by making minute changes in fuel flow, this method is time consuming.<br />

On the one h<strong>and</strong>, if the fuel flow is increased too rapidly than<br />

excessive combustor heat is generated <strong>and</strong> either the turbine inlet<br />

temperature will be exceeded or the increase in speed will drive<br />

the compressor into surge, or both. On the other h<strong>and</strong> if the fuel<br />

flow is decreased too rapidly then the reduction in fuel flow could<br />

be faster than the rate at which the compressor will reduce airflow<br />

<strong>and</strong> pressure <strong>and</strong> result in a flame-out or compressor surge (as speed<br />

decreases the compressor operating point moves closer to the surge<br />

line). High turbine inlet temperature will shorten the life of the turbine<br />

blades <strong>and</strong> nozzles, <strong>and</strong> compressor surge could severely damage<br />

the compressor blades <strong>and</strong> stators (<strong>and</strong> possibly the rest of the gas<br />

turbine). Flame-out as a result of power decease takes its toll in the<br />

long run because of the thermal stresses created with each shutdown<br />

<strong>and</strong> re-start.<br />

The control must also guard against surge during rapid power<br />

changes, start-up, <strong>and</strong> periods of operation when compressor inlet<br />

temperature is low or drops rapidly. Note: the gas turbine is more<br />

susceptible to surge at low compressor inlet temperatures. Normally<br />

changes in ambient temperature are slow compared to the response<br />

time of the gas turbine control system. However, the temperature<br />

range from 28°F (–2.0°C) to 42°F (6.0°C) accompanied with high humidity<br />

is of major concern. Operation in this range has resulted in ice<br />

formation in the plenum upstream of the compressor. To address this<br />

problem, anti-icing schemes have been employed to increase the sensible<br />

heat by introducing hot air into the inlet. Anti-icing, therefore,<br />

becomes another control function that must address both the problem<br />

of ice formation, as well as the effect temperature changes have on<br />

the compressor relative to surge.<br />

The acceleration schedule facilitates loading the unit as quickly<br />

as possible. Without the acceleration schedule it would be very time<br />

consuming to increase the load from the Idle-No-Load position to the<br />

Full-Load position. As prescribed by the acceleration schedule, the<br />

fuel valve is opened <strong>and</strong> loading is initiated. As load approaches its<br />

target set point the speed governor starts to override the acceleration

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